DocumentCode :
236666
Title :
Electric powered airplane VUT 051 RAY
Author :
Cervinka, Dalibor ; Knobloch, Jan ; Prochazka, Petr ; Kadlec, Josef ; Cipin, Radoslav ; Pazdera, Ivo
Author_Institution :
Brno Univ. of Technol., Brno, Czech Republic
fYear :
2014
fDate :
3-5 Dec. 2014
Firstpage :
6
Lastpage :
10
Abstract :
The paper deals with a drive system of experimental fully electric airplane VUT 051 RAY with rated power 55 kW. The requirements on accumulator capacity and its weight were defined according to a precisely specified flight profile. The whole design process of traction inverter is presented. Drive train system of electric airplane was completely tested, before its final installation into fuselage of airplane. Measured parameters gained by testing are presented too. Finally, the results of first flight are presented.
Keywords :
aircraft; electric drives; invertors; secondary cells; traction; accumulator capacity; airplane fuselage; electric powered airplane VUT 051 RAY drivetrain system; power 55 kW; traction inverter; Airplanes; Batteries; Inverters; Permanent magnet motors; Synchronous motors; Temperature measurement; Traction motors; DC/AC inverter; Li-Ion battery; electric airplane;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Mechatronics - Mechatronika (ME), 2014 16th International Conference on
Conference_Location :
Brno
Print_ISBN :
978-80-214-4817-9
Type :
conf
DOI :
10.1109/MECHATRONIKA.2014.7018228
Filename :
7018228
Link To Document :
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